Number | Title | Status | Office | Date |
---|---|---|---|---|
33.70-2 |
Damage Tolerance of Hole Features in High-Energy Turbine
This advisory circular (AC) provides definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with requirements in § 33.70 of Title 14 of the Code of Federal Regulations related to the integrity of engine life-limited parts. |
Active | AIR-600 | 2009-08-28 |
33.70-1 |
Guidance Material for Aircraft Engine Life-Limited Parts Requirements
This advisory circular (AC) provides definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the engine life-limited parts integrity requirements of § 33.70 of Title 14 of the Code of Federal Regulations (14 CFR part 33). |
Active | AIR-600 | 2009-07-31 |